Airworthiness Directive 55-14-02

one-time
AD 55-14-02 · 1955-01-01 · airframe

Airworthiness Directives; modified as follows: 1. If the cylinder housing is upset or fractured, it must be replaced by a new reinforced cylinder P/N 455927

Which aircraft AD 55-14-02 applies to

MakesPiper
Part-conditional455927.

Cylinder housing inspection/replacement per Piper Service Bulletin No. 138; replacement reinforced cylinder P/N 455927 (applicability read from the AD teaser — confirm exact model/serial from the records.)

Whether AD 55-14-02 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 55-14-02 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

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Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.